Piston for an internal combustion engine
A piston for an internal combustion engine with a piston crown and a circumferentially arranged crown edge, whereby, near the periphery of the crown edge, a thermal barrier coating is applied, whereby the thermal barrier coating tapers off before the periphery of the crown edge.
1. A piston for an internal combustion engine with a piston crown and a circumferentially arranged crown edge, wherein, near the periphery of the crown edge, a thermal barrier coating is applied, wherein the thermal barrier coating tapers off before the periphery of the crown edge, wherein the thermal barrier coating extends in a radial direction relative to a center of the piston crown from the center of the piston crown toward the crown edge, and wherein the thermal barrier coating extending in the radial direction on the piston crown near the crown edge is located at a radial position (r) spaced from the center of the piston crown that begins, away from the center of the piston crown, 80% of a distance between the crown edge and the center of the piston crown.
2. The piston according to claim 1 , wherein the thermal barrier coating comprises a cover layer and an adhesion promoter layer, wherein the cover layer is arranged on the adhesion promoter layer and the adhesion promoter layer is arranged on the crown edge.
3. The piston according to claim 2 , wherein the cover layer of the thermal barrier coating comprises ceramic.
4. The piston according to claim 2 , wherein the adhesion promoter layer of the thermal barrier coating consists of a metal alloy.
5. The piston according to claim 1 , wherein the thermal barrier coating has a decreasing thickness (d) in the direction of the center of the piston crown.
6. The piston according to claim 5 , wherein a fire land area of the piston is free of the thermal barrier coating.
7. The piston according to claim 6 , wherein in a fire land area of the piston near the piston crown, a plurality of grooves are arranged.
8. An internal combustion engine, comprising at least one piston according to claim 1 .
9. The piston according to claim 1 , wherein the thermal barrier coating is annular shaped and has an inner perimeter and an outer perimeter, and the thermal barrier coating tapers both in the radial direction towards the inner perimeter and in the radial direction towards the outer perimeter.